Equipment: Engine(s) Details: ENGINE Lycoming IO-540V-V4A5 max power 260 hp / 194 kW WEIGHTS AND DIMENSIONS max take off mass, MTOM 1315 kg / 2900 lb (subject to extension to 1360 kg / 3000 lb) useful payload 500 kg / 1100 lb total usable fuel 2 x 105 l / 2 x 27.7 gal full fuel payload 350 kg / 770 lb PERFORMANCE (at MTOM) stall speed (flaps extended), VS0 55 KIAS stall speed (flaps retracted), VS 60 KIAS maneuvering speed, VA 143 KIAS never exceed speed, VNE 220 KIAS Performance cruise speed at 75% power 198 KTAS, FL 80 climb rate at MTOM and VY 6.6 m/s / 1300 ft/min take off ground roll 372 m / 1220 ft take-off distance (50 ft obstacle) 657 m / 2155 ft landing distance (50 ft obstacle) 706 m / 2316 ft landing ground roll 346 m / 1135 ft fuel consumption at 75% power 56 l/h / 14.8 gal/h range (with 45 min reserve) > 1000 nm, 155 KTAS, FL 120, 4 people aboard (4 x 86 kg) ceiling 7600 m / FL250

Avionics: Avionics: Garmin G3X GDU 460 dual 10-inch display PFD and MFD (dual ADAHRS, Synthetic Vision, EMS, ARINC module) Garmin GMC 307 2-axis GPS-slaved digital autopilot Garmin GTN 750 Xi Com/Nav/IFR GPS, touch screen Garmin GTN 650 Xi Second Com/NAV/IFR GPS, touch screen Garmin GMA 35 Remote Audio Panel, Intercom Garmin GTX 345R Transponder Mode C/S ES ADS-B In/Out Artex ELT 345 (406 MHz) Mid-Continent Instruments SAM Backup Airspeed, Backup Altimeter, Backup Artificial Horizon